Showing posts with label MECHANICAL ENGINEERING – 2003. Show all posts
Showing posts with label MECHANICAL ENGINEERING – 2003. Show all posts

Monday, 23 February 2015

MECHANICAL ENGINEERING – 2003,PAPER – II ,Section B

                    Time Allowed: Three Horus      Maximum marks: 200
Candidates should attempt Questions 1 and 5 which are compulsory and any THREE of the remaining questions selecting at least ONE question from each Section.
If any data is considered insufficient, assume suitable valur.
  
SECTION B
5.       Answer any four parts:

(a)    The evaporator and condenser temperatures in a reverse Carnot refrigeration cycle of 1 TR capacity are 263 K and 313LK respectively. The outlet of compression is saturated vapour and into to turbine is saturated liquid. Find the mass flow rate, work done condenser heat rejection and COP. Properties of refrigerant at saturation in SI units are as follows:

t (K)
hf
hg
S f
Sg
263
154.056
1450.22
0.82965
5.755
313
390.587
1490.42
1.64377
5.1558

(b)   Air enters a cooling coil at 30˚C, 75 % relative humidity. The apparatus dewpoint is 12˚ c and bypass factor is 0.15. Find the temperature and humidity ratio at outlet of cooling coil. If mass flow rate of air is 10 kg / s, find the condensate rate and cooling capacity of cooling coil. The partial pressures of water vapour at 12˚ C and 30˚C are 1.4017 and 4.2431 kPa respectively. Atmospheric pressure is 101.325 kPa. Enthalpy of condensate at 12˚C = 50.24 kJ / kg.
(c)    Explain the nomenclature Rabc for CFCs and inorganic compounds. What is meant by ozone depletion? Name at least two refrigerants that do not cause it.
(d)   State Buckingham’s  theorem. Using Buckingham’s  theorem obtain an expression for drag force on a partially submerged body moving with a relative velocity V in fluid, the other variables being linear dimension L height of surface roughness K, the fluid density ƿ and gravitational accelerating.
(e)   Discuss the criteria for the selection of site for steam and hydroelectric power plants.

6.       (a) A refrigeration system of 10 TR cooling capacity has condenser and evaporator temperatures of 45˚C and – 20 ˚C respectively. The vapour leaving the evaporator sub cools the liquid leaving the condenser from 45 ˚C to 25˚C. Draw schematic diagram and T.S fiagram considering isentropic compression, isobaric heat absorption and rejection. Determine mass flow rate, compressor work. Condenser heat rejection and COP. Use vapour specific heat at condenser pressure to find COP. USE vapour specific heat at condenser pressure to fin adiabatic discharge temperature and enthalpy. The properties in SI units at saturation are:


hf
hg
sg
C pg
Cpf
-20˚ C
17.8
178.7
0.7088
0.61
-
45˚C
79.7
204.9
0.6812
0.755
1.02

                        (b) Define thermodynamic wet bulb temperature t* and show that humidity ratio may be expressed as

W = W* h* fg  - 1.005 (t- t*)    /   hg (t) – h*f

Where enthalpy of moist air is expressed as h= 1.005 (t) + hg (t).

7.       (a)  Diabatic flow of dry air takes place through a frictionless constant area duct. At some particular section of the duct, the Mach number is 4.0 while stagnation temperature and static pressure are 280 K and 0.5 bar respectively. Calculate the stagnation temperature. Static and stagnation pressures at a section where the Mach numbers is 2.0 also find the amount of heat transfer which causes this reduction Mach number. Take Cp= 1.005 kJ/ kg and γ = 1.4.
M
P /ᵖP*
T/ T*
Tₒ/ Tₒ*
Pₒ / Pₒ*

2.0
0.364
0.529
0.793
1.503
4.0
0.1026
0.168
0.589
8.277
  
                                                                                                                 
          (b) Explain what you understand by specific speed of a turbo machine. Give its importance.
Calculate the specific speeds of the following cases:

             (i)                  A 2500 kW gas turbine is running at a speed of  18000 RPM. The entry and exit conditions of the gas are T₁ = 1100 K₁ P₁ =60 bar, P₂ = 30 bar.
            (ii)                A centrifugal compressor develops a pressure ratio of 1.5 while running at 24000 RPM and discharging 2.0 kg/s of air, the entry conditions are P₁ =1.0, T₁ = 290K.
1 or both cases take
γ + 1.4, R = 287 J / kg – k, Cᵨ =1.005 kJ / kg –k.

8.       (a) Explain clearly, “heat rate curve’ and “ Incremental rate curve’. Show that the incremental rate curve crosses the heat rate curve at the lowest value of heat rate.
The incremental fuel costs for two generating units A and B of a plant are given by
dF a / dPa  = 0.065 Pa + 25
dF b / dPb = 0.08 Pb + 20
where F is fuel cost in Re / hr and P is power output in MW. Find –

(i)                  The economic loading of the two units when the total load supplied by the power plant is 160 MW.
(ii)                The loss in fuel cost/ hr if the load is shared equally by the units.

(b) Discuss the importance of the terms, capacity factor and use factor from the economic point of view of the power plant.

A power station is said to have a sue factor of 50% and a capacity factor of 45%. How many hours the plant did not operate during the year?

MECHANICAL ENGINEERING – 2003,PAPER – II ,Section A

                              Time Allowed: Three Horus      Maximum marks: 200
Candidates should attempt Questions 1 and 5 which are compulsory and any THREE of the remaining questions selecting at least ONE question from each Section.
If any data is considered insufficient, assume suitable valur.

Newton may be converted to kg using the equality 1 kolonewton (1 kN) = 100 kg, if found necessary.
All answers should be in SI units.
Take: 1 kcal = 4. 187 kJ and 1 kg /cm³ = 0.98 bar
1 bar = 10⁵ Pascals
Universal gas constant = 8314.6 J/ k mol – k

Section A
1.       Answer any four parts:

(a)    (i) Two cannot engines work in series between the source and sink temperatures of 600 K and 300 K, if both engines develop equal power, determine the intermediate temperature.
               (ii) Show that the compression ratio for the maximum work to be done per kg of air in an Otto cycle between upper and lower limits of absolute temperatures T₃ and T₁ is given by the expression
R= (T₃ / T₁)    1 / 2(γ-1) 
(b)   (i) An ideal gas is heated at constant volume until its temperature is 3 times the original temperature, then it is expanded isothermally till is reaches its original pressure, the gas is then restored to its original state. Determine the expression of net work done.
               (ii) 300 kj / sec of heat is supplied at a constant fixed temperature of 290˚C to a heat engine. The heat rejection takes place at 8.5˚C. The following results were obtained:
                              (I)                 215 kJ/ s of heat is rejected
                             (II)               150 kJ/ s of heat is rejected
                            (III)             75 kJ/ s of heat is rejected
Using Clausius inequality which of the results report a reversible cycle of irreversible cycle, or impossible result? 
(c)    (i) What is petrol injection? What are its advantages and disadvantages?
                  (ii) What is petrol injection? What are its advantages and disadvantages?

(d)   Make a detailed comparison of SI and CI engines with respect to basic cycle, fuel, introduction of fuel in the cylinder, ignition, compression ratio and weight.

(e)   Two parallel flat plates of equal area 0.5 m² each face each other. These are at 1000 K and 500 k respectively. Shape factor between them F₁₂ = F ₂₁ = 0.285. These are placed in room whose walls are at 300 k. Find radiation heat transfer rate between the plates and between the plates and wall. Assume that outer part of both the plates is insulated.
Stefan- Boltzmann constant = 5.67 x 10 ⁻⁸ W/ K ⁴ - m³.

2.       (a) What is detonation? Factors leading to increase detonation in SI engines tend to reduce knock states above in the light of differences in their nature. Indicate the methods to reduce knock in CI engines.

(b) Determine the diameter of a fuel orifice for a 4-stroke engine working on diesel cycle developing 18 kg/ kw-hr fuel of 30˚ API. The duration of the crank injection is 30˚ of crank travel the fuel injection pressure is 125 bars and the combustion chamber pressure is 35 bars. Take velocity coefficient as 0.9 and
Ƿ = 141.5 / 131.5 + ˚API

3.       (a) (i) What is stoichiometric air requirement and excess air factor?

                                   (ii) What do you understand by higher calorific value and lower calorific value?   Explain the methods to measure them
                            (b) Determine the air-fuel ratio at 6000 m altitude in a carburetor adjusted to give an air-fuel ratio of 15: 1 at sea level where the air temperature is 300 k and pressure of 1.013bar.
The temperature of air decreases with altitude and is given by the expression

t =ts – 0.0065 h.
Where h is altitude in meters and ts is the temperature at sea level in ˚C.
The air pressure decreases with altitude as per the relation
 H= 19220log 10 (1.013 /P)
Where, p is in bar.
What remedies would you suggest to compensate for the decrease in air fuel ratio at high altitudes? Discuss them giving justification

4.       (a) show that the governing equation for temperature distribution in a fin of uniform cross –section is given by

d² Ѳ/ dx² - m² Ѳ = 0
Where, Ѳ = T – T, and m² = hP/ kA.
Further, show that the solution for boundary conditions Ѳ = Ѳₒ at X = 0 and Ѳ = Ѳ ₁at x = L is
Ѳ = [Ѳ₁ sin h mx + Ѳₒ sin h m (L – X)] / sin h mL.

                           (b) Water flows in the tube and brine flows in the annulus of a double –tube heat exchanger. Water at the rate of 0.015 kg/s is cooled from 30˚ C to 20˚C and temperature of brine increases from - 15˚C to - 5˚C. The inner and outer diameters of water of water-carrying tube are 25mm and 30 mm respectively, and thermal conductivity of metal is 45 W/ m –K. The convective heat transfer coefficients on the brine and water, side are 2700 and 2100 W/ m² - K respectively. Find 

 Overall heat transfer coefficient and then the length of the heat exchanger for parallel flow and counter flow and counter flow. Specific heat of water = 4.18kJ / kg –k.